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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1952
 Serial/Series Title: NACA Technical Notes
 Collection: National Advisory Committee for Aeronautics Collection
Abnormal grain growth in S-816 alloy

Abnormal grain growth in S-816 alloy

Date: April 1, 1952
Creator: Rush, A I; Freeman, J W & White, A E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Accuracy of approximate methods for predicting pressures on pointed nonlifting bodies of revolution in supersonic flow

Accuracy of approximate methods for predicting pressures on pointed nonlifting bodies of revolution in supersonic flow

Date: August 1, 1952
Creator: Ehret, Dorris M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Achievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles

Achievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles

Date: January 1, 1952
Creator: Evvard, J C & Marcus, Lawrence R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes

Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes

Date: June 1, 1952
Creator: Riebe, John M & Naeseth, Rodger L
Description: An investigation was made in the Langley 300-mph 7- by 10-foot tunnel to determine the aerodynamic characteristics of a refined deep-step planing-tail hull with various forebody and afterbody shapes and, for comparison, a streamline body simulating the fuselage of a modern transport airplane. The results of the tests indicated that the configurations incorporating a forebody with a length-beam ratio of 7 had lower minimum drag coefficients than the configurations incorporating a forebody with length-beam ratio of 5. The lowest minimum drag coefficients, which were considerably less than that of a conventional hull and slightly less than that of a streamline body, were obtained on the length-beam-ratio-7 forebody, alone and with round center boom. Drag coefficients and longitudinal- and lateral-stability parameters presented include the interference of a 21-percent-thick support wing.
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of three deep-step planing-tail flying-boat hulls and a transverse-step hull with extended afterbody

Aerodynamic characteristics of three deep-step planing-tail flying-boat hulls and a transverse-step hull with extended afterbody

Date: August 1, 1952
Creator: Riebe, John M & Naeseth, Rodger L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section

The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section

Date: June 1, 1952
Creator: Beckwith, Ivan E; Ridyard, Herbert W & Cromer, Nancy
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The aerodynamic design of supersonic propellers from structural considerations

The aerodynamic design of supersonic propellers from structural considerations

Date: December 1, 1952
Creator: Hammack, Jerome B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range

Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range

Date: September 17, 1952
Creator: Chapman, Dean R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics

Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics

Date: June 1, 1952
Creator: Jones, Arthur L & White, John S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of flow in a subsonic mixed-flow impeller

Analysis of flow in a subsonic mixed-flow impeller

Date: August 1, 1952
Creator: Wu, Chung-Hua; Brown, Curtis A & Costilow, Eleanor L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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